C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics

C04B35/16—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay

C04B35/18—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on silicates other than clay rich in aluminium oxide

Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Abstract

A fibrous ceramic material comprises a plurality of fibers having a RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure. The fibrous ceramic material is form by combining two or more RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursors in which at least one of the two or more RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursors is in fiber form. The fibrous ceramic material is shaped to form a fibrous body in which at least about 20% of all fibers therein are aligned in a substantially common direction.

The invention generally relates to a fibrous ceramic material, and more particularly to a low coefficient of thermal expansion fibrous material including a plurality of nonstoichiometric cordierite fibers and methods of manufacturing the fibrous material.

BACKGROUND

Advanced ceramic materials are commonly utilized in systems located in hostile environments, such as, for example, automotive engines (e.g., catalytic converters), aerospace applications (e.g., space shuttle titles), refractory operations (e.g., firebrick) and electronics (e.g., capacitors, insulators). Porous ceramic bodies are of particular use as filters in these environments. For example, today's automotive industry uses ceramic honeycomb substrates (i.e., a porous ceramic body) to host catalytic oxidation and reduction of exhaust gases, and to filter particulate emissions. Ceramic honeycomb substrates provide high specific surface area for filtration and support for catalytic reactions and, at the same time, are stable and substantially structurally sound at high operating temperatures associated with an automotive engine environment.

In general, ceramic materials, such as for example, cordierite, are inert materials that perform well in high temperature environments. However, ceramic materials are not immune to thermal stresses, such as those stresses generated from cycling between ambient temperature and high temperature applications. Thus, ceramic filters are known to degrade making them inefficient and ineffective for today's applications.

SUMMARY OF THE INVENTION

In general, embodiments described herein feature a fibrous ceramic material that can be utilized in a variety of applications, including as a filter in an automotive engine environment. The fibrous ceramic material includes a plurality of nonstoichiometric cordierite fibers (i.e., fibers having a compositional structure of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 where x is greater than 0 and R is an element other than Mg, Al, Si, or O). Embodiments described herein also feature methods of making the fibrous ceramic material. Specifically, in one embodiment, the fibrous ceramic material is made by forming the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers via a reaction between two or more precursor materials, wherein at least one of the two or more precursor materials is in the form of a fiber. The plurality of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers made by reaction are extruded or otherwise shaped into a fibrous body. During extrusion or shaping, it is believed that fiber alignment occurs resulting in a decrease of the coefficient of thermal expansion (CTE) in at least one direction of the fibrous body. As a result of the decrease in CTE, a porous, fibrous ceramic body with minimal cracking and minimal expansion at high temperatures can be generated. In addition, in certain embodiments, the CTE can be further lowered by changing the compositional structure of the fibers. For example, by altering the compositional structure of cordierite from its stoichiometric form, one can manipulate the crystal lattice of the fibrous material resulting in directional changes to the value of the CTE.

In one aspect, embodiments described in the present disclosure are directed to a method of manufacturing a fibrous material wherein at least about 5% of all fibers within the fibrous material have either RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure. The method includes mixing at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a mixture (one or more of the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors being in the form of a fiber); extruding the mixture to create a fibrous body; and heat treating the fibrous body to form the fibrous material.

Embodiments of this aspect of the invention can include one or more of the following features. In some embodiments after heat treating the fibrous body at least about 25% of all fibers therein have one of the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure. That is about 25% (e.g., 30%, 35%, 45%, 55%, 65% or more) of the precursor fibers reacted to form either RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers. In certain embodiments, one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers. The mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.

In another aspect, embodiments described herein are directed to a method of manufacturing a fibrous body including RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers. The method includes mixing at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is in the form of a fiber; reacting the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a plurality of fibers within the mixture that have RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure; and shaping the mixture into the fibrous body, wherein at least about 5% of all fibers within the fibrous body have either the RxMg2Al4+2xSi5−xO18 compositional structure or the RxMg2−xAl4Si5O18 compositional structure.

Embodiments of this aspect of the invention can include one or more of the following features. In some embodiments at least about 25% of all fibers within the fibrous body after reacting the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials have the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure. That is, at least 25% (e.g., 35%, 45%, 55%, 65%, 75%, 85%, 95%) of all the fibers within the fibrous body after the reaction of the precursors have either the RxMg2Al4+2xSi5−xO18 compositional structure or RxMg2−xAl4Si5O18 compositional structure. The fibers can be aligned such that at least about 20% of all of the fibers within the fibrous body are aligned in a common direction. In certain embodiments, one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers. The mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.

In yet another aspect, embodiments of the invention are directed to a method of forming a porous honeycomb substrate. The method includes mixing at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is in a form of a fiber; extruding the mixture to form a honeycomb substrate having a porosity of at least about 20%; and heat treating the honeycomb substrate to react the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a plurality of fibers having RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure so that at least about 5% of all fibers within the honeycomb substrate have the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure.

Embodiments of this aspect of the invention can include one or more of the following features. In some embodiments after heat treating the honeycomb substrate at least about 25% of all fibers therein have one of the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure. The fibers can be aligned such that at least about 20% of all of the fibers within the fibrous body are aligned in a common direction. In certain embodiments, one or more of the precursor materials can be selected from the group consisting of magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers. The mixture can, in some embodiments, further include one or more additives selected from the group consisting of a fluid, a binder, and a pore former. The one or more additives can be substantially removed by heating the fibrous body.

In another aspect, embodiments are directed to a RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibrous honeycomb body. The fibrous honeycomb body including a honeycomb array of walls defining channels between adjacent walls. The walls include a plurality of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers bonded to form a porous structure having an open network of pores. About 20% of the plurality of fibers within the walls are aligned in a common direction.

Embodiments of this aspect can include one or more of the following features. The walls within the fibrous honeycomb body can have a porosity of at least about 20% (e.g., 25%, 30%, 35%, 40%, 45%, 50%). In some embodiments, the plurality of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers have an aspect ratio greater than about 1 and less than or equal to 2,000. In certain embodiments, a catalytic coating is disposed on the plurality of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers.

In another aspect of the invention, embodiments are directed to a filter. The filter includes a housing including an inlet and an outlet. Disposed between the inlet and the outlet is a RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibrous honeycomb body. The body includes a honeycomb array of walls defining channels between adjacent walls. The walls include a plurality of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers bonded to form a porous structure having an open network of pores. In some embodiments the fibers within the walls are aligned in a common direction. In certain embodiments, at least one catalyst is deposited on the plurality of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers.

BRIEF DESCRIPTION OF THE DRAWINGS

In the drawings, like reference characters generally refer to the same parts throughout the different views. Also, the drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the invention.

FIG. 1 is a flow chart illustrating a method of forming a fibrous material in accordance with an embodiment of the disclosure.

FIG. 2 is a micrograph a portion of a fibrous material formed in accordance with the method of FIG. 1.

FIGS. 3 A and 3B are cross-sectional schematics illustrating the presence and the absence of pore formers and binders prior to and after a heat treatment, respectively.

FIG. 4 is a flow chart illustrating another method of forming a fibrous material in accordance with an embodiment of the disclosure.

FIG. 5 is a schematic illustrated in a perspective view showing a honeycomb body.

FIG. 6 is a schematic illustrated in a perspective view showing multiple honeycomb bodies to be adjoined to form a larger body.

FIG. 7 is a cross-sectional schematic of a filter that includes a honeycomb body of FIG. 5.

FIG. 8 is a schematic illustrating a method of forming a honeycomb body in accordance with an embodiment of the disclosure.

DETAILED DESCRIPTION

In general, by reducing a ceramic material's CTE value, cracking due to thermal stresses can be minimized. The ceramic materials described below have a low CTE value. It is believed that the low CTE value is achieved by one or more of: (1) a substantial alignment of fibers within the material, (2) a manipulation of one or more of the lattice parameters through an adjustment in compositional structure of the ceramic material or (3) a combination of the alignment process of (1) and the manipulation of one or more of the lattice parameters as described in (2) above.

The ceramic materials described herein can be utilized in numerous applications, including but not limited to filters for diesel applications. In diesel automotive applications, using ceramic materials that have a high coefficient of thermal expansion within a catalytic filter can lead to poor or diminished performance and/or design flexibility. Specifically, diesel filters are prone to cracking during regeneration (i.e., a high temperature cycle used to burn out particulates trapped in the filter). Therefore, it would be advantageous to minimize the coefficient of thermal expansion of a ceramic material used in a diesel filter. In addition, performance of a diesel filter increases with an increased value for the thermal shock parameter (TSP). The thermal shock parameter is defined as follows: TSP=modulus of rupture (MOR) divided the product of Young's modulus and the coefficient of thermal expansion (CTE). As a result, a ceramic material having a low coefficient of thermal expansion will have greater performance.

Referring to FIG. 1, a method 100 for manufacturing a fibrous ceramic material is illustrated. The fibrous ceramic material formed using this method has an ultimate or final structure (i.e., a structure after completion of the method shown in FIG. 1) in which at least about 5% of all fibers therein have either the RxMg2Al4+2xSi5−xO18 or the RxMg2−xAl4Si5O18 compositional structure. The fibers within the final structure are interlocking, so as to form a three dimensional porous structure in which fluids (e.g., gases) can pass therethrough. The method includes mixing at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials, such as a first precursor 105 and a second precursor 107 to form a mixture 120. (While FIG. 1, shows two precursors, any number of precursors greater than or equal to two can be utilized.) A RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursor is a material that when reacted with other materials forms a portion of the RxMg2Al4+2xSi5−xO18 or the RxMg2−xAl4Si5O18 compositional structure, respectively. For example, a possible RxMg2Al4+2xSi5−xO18 precursor is Veegum clay (i.e., a clay that includes MgO, SiO, and Al2O3); another possible precursor is Al2O3 powder; another possible precursor is a sol of any material including Mg, Al, and/or Si; still yet another precursor is GeO where R in RxMg2Al4+2xSi5−xO18 represents Ge. (The above RxMg2Al4+2xSi5−xO18 precursors are also RxMg2−xAl4Si5O18 precursors.)

Precursors 105 and 107 can come in a number of forms. For example, the precursors can be fiber based, colloidal based, particle/powder based, or liquid solution based. However, one or more of the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors (i.e., 105 and 107) is in the form of a fiber so that mixture 120 is a fiber based material. That is, at least one of precursor 105 and precursor 107 is in the form of a fiber, such as, for example, alumina fibers, silica fibers, mullite fibers, alumina silicate fibers (e.g., Al2O3SiO2 fibers, mullite fibers, cordierite fibers), magnesium aluminate fibers, or magnesia silica fibers.

Optionally, additives 110, such as, for example binders, rheology modifiers (e.g., fluids), and pore formers can be introduced into mixture 120. These additives 110 can be used to modify or manipulate the consistency of mixture 120 so as to aid in later form shaping processes. In addition, these additives 110 can be used as pore place holders. That is, these additives are inert with respect to the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors and can be removed from the mixture 120 after the form shaping processes, thereby allowing for increased porosity in the ultimate form.

After the RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursors (i.e., 105 and 107) with any optional additives 110 are mixed and homogenized, the mixture 120 is shaped 130 into a form. In one embodiment, shaping 130 can occur by extrusion of the mixture 120. Without wishing to be bound by theory, it is believed that extrusion of a fibrous mixture, such as mixture 120, results in the substantial alignment of fibers. For example, it is believed that at least about 20% of the fibers within a fibrous mixture are substantially aligned in a common direction after extrusion. FIG. 2 shows an extruded fibrous structure 175 in which an average of 80% of all fibers within the form are aligned along line a-a shown therein. Shear forces that act upon the mixture during extrusion tend to orient the fibers in the direction of extrusion. It will be appreciated that extrusion designs, mixture rheologies, and fiber content and fiber rigidity can influence the orientation behavior of the extruded mixture.

Other shaping processes 130, other than extrusion, can also be utilized to create the form. Examples of other shaping processes include molding, such as injection molding, and casting. In these shaping processes, fiber alignment may occur to a lesser degree than with extrusion.

Once shaped, energy is applied to the form to initiate a reaction 140 between the precursors 105 and 107. For example, the form can be fired at a temperature of less than about 1,420° C. for several hours to cause a reaction between the two or more RxMg2Al4+2xSi5−xO18 precursors or two or more RxMg2−xAl4Si5O18 precursors. As a result of this reaction, at least 5% of all fibers within the form are transformed into either RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers. For example, if the RxMg2Al4+2xSi5−xO18 precursors included mullite fibers, MgCO3 particles, and GeO2 particles, under the influence of heat, 5% or more of the fibers therein are transformed to have the following compositional structure: GexMg2Al4+2xSi5−xO18 (where x will be dependent on the relative ratios of the precursors used). The application of energy (e.g., heat) also allows for the creation of bonds between the fibers. As heat is applied (e.g., directly in the case of a furnace or inductively as when an RF source is utilized), water and other additives are eliminated or reduced resulting in fiber-to-fiber contact. (See FIGS. 3A and 3B showing fiber 300 interactions as a result of the presence and the removal of pore formers 305 and binders 310, respectively). It will be appreciated that the bonds may be formed in several ways at these fiber-to-fiber contact sites. For example, a number of types of sintering mechanism can be utilized, including but not limited to liquid assisted sintering, solid state sintering, and reaction-phase sintering wherein a chemical reaction occurs at the fiber-to-fiber contact site. As a result of fiber bond formation, the ceramic material formed utilizing method 100 is a fibrous material having interlocked fibers, wherein at least 5% of all fibers have the either RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure.

As an optional step, the fibrous form can be further processed as shown in step 150 in FIG. 1. Further processing steps include: (a) additional heat treatments to create further bonds between fibers or to remove additives such as pore formers, organic binders, and fluids, such as water (b) application of coatings, such as, for example catalytic coatings on the fibers, (c) introduction of increased porosity or creation of directed flow channels via mechanical processing (e.g., drilling or capping/filling passageways), and (d) incorporating the fibrous material into a filter or other apparatus.

In another embodiment, shown in FIG. 4, a method 200 of forming a fibrous body includes mixing at least two RxMg2Al4+2xSi5−xO18 precursors or RxMg2−xAl4Si5O18 precursors (205 and 207) together with any optional additives 210 to form a mixture 220. One or more of the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors 205 and 207 is in fiber form. Energy, such as heat or light, is applied to the mixture to initiate a reaction 230 between the two or more RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors. The optional additives 210 are inert with respect to the precursors 205 and 207, and as a result do not participate in the reaction. The reacted mixture 230 is then shaped 240 into the fibrous body through extrusion, molding, or other shaping technique. Optional processing steps 250, such as, for example, heat treating the fibrous body to remove or reduce the amount of optional additives 210, sintering the fibrous body to create bonds between fibers, introducing further porosity or directed flow channels into the fibrous body, depositing coatings, and/or incorporating the fibrous material into a filter or other apparatus can be performed after the fibrous body is shaped 240.

The RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors utilized in methods 100 and 200 can be supplied in various forms. As discussed above, one or more of the at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors is in the form of a fiber so that any resulting mixture of the precursors is a fiber based material. An illustrative list of RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors in fiber form includes, but is not limited to: alumina silicate fibers, such as for example, mullite fibers, aluminosilicate H95C fibers, strontium aluminum silicate fibers, lithium aluminum silicate fibers, and aluminoborosilicate fibers, magnesium silicate fibers, such as, for example Isofrax fibers (a biosoluble fiber available from ISOFRAX, Niagara Falls, N.Y.), magnesium strontium silicate fibers, and magnesium calcium strontium silicate fibers, Al2O3 fiber, SiO fibers, MgO fibers, Li2O fibers, where R is Li, and SrCO3 fibers where R is Sr. In general, these fibers have an aspect ratio (i.e., the ratio of the length of the fiber divided by the diameter of the fiber) greater than one. As used herein, the “diameter” of the fiber assumes for simplicity that the sectional shape of the fiber is a circle; this simplifying assumption is applied to fibers regardless of their true section shape (e.g., square, triangular, etc.) In certain embodiments, the fibers have an aspect ratio that is less than or equal to 2,000. That is, in certain embodiments, the fibers have a diameter in the micron or submicron range (e.g., 1 micron) while the length of the fibers is a few millimeters (e.g., 2 millimeters). In general, the fibers can have a diameter ranging from about 100 nm to about 100 microns. However, in certain embodiments, the fibers have a diameter within the range of about 100 nm to about 10 microns and in some embodiments, the fibers have a diameter within the range of about 2 microns to about 10 microns.

The at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors can be all in fiber form or alternatively, the precursors can be any combination of fibers and some other form. Other RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors, which are not in fiber form, include but are not limited to: MgCO3 particles, colloidal silica, silica particles, Al2O3 particles, sols of any material including Mg, Al, or Si, Veegum clays, talcs, or particles, SrCO3 particles where R is Sr, GeO2 particles where R is Ge, K2O particles where R is K, LiO where R is Li, and MnO particles where R in Mn. The above list of precursors is for illustrative purposes only and is by no means exhaustive. That is, any precursor material that when reacted with other constituents forms a portion of a RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fiber can be utilized in methods 100 and 200.

The specific RxMg2Al4+2xSi5−xO18 precursors or RxMg2−xAl4Si5O18 precursors and precursor amounts utilized are selected in accordance with a target fiber chemistry and crystal structure. That is, the amount and type of precursor 105/205 and the amount and type of precursors 107/207 are selected based on the target fiber chemistry and crystal structure. For example, if a targeted fiber chemistry is CaxMg2Al4+2xSi5−xO18 having a cordierite type crystal structure (i.e., orthorhombic crystal structure), then the following four RxMg2Al4+2xSi5−xO18 precursors having the following weight percents could be used: 71.2% aluminosilicate fiber:21.9% Isofrax fiber:5.3% MgCO3 particles:1.5% CaCO3 particles. Similarly if the same target fiber chemistry (i.e., CaxMg2Al4+2xSi5−xO18) is desired but instead of an orthorhombic crystal structure a triclinic or anorthite crystal structure is desired, then the following weigh percents of the precursors can be utilized: 62% aluminosilicate fiber:18% Isofrax fiber:6.9% MgCO3 particles:12.5% CaCO3 particles. By lowering the amount of Al but increasing the amount of Ca available during the reaction, a different crystal structure forms and thus different lattice parameters and associated properties are achieved. As a result, the fiber chemistry and crystal structure can be tailored to achieve optimum properties for a specific application.

In addition to determining the crystal structure of the resulting fiber, the relative amounts of the at least two precursors also affects the amount of precursor fibers that participate in reaction 140/230. In order for all or substantially all of the precursor material to participate in the reaction 140/230 the relative amounts of the precursors should be substantially equal to their solubility limits for a particular solid solution having a particular crystal structure. If the relative amounts vary from the solubility limit but are still within a range therein to form a particular crystal structure, then the reaction can be limited due to a shortage of one or more elements. As a result, not all of the precursor fibers will participate in the reaction and thus some precursor fibers will remain in the fibrous body after reaction 140/230 has taken place. Accordingly, the fibrous body can include less than 100% RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers. For example, about 45% of the fibers within a fibrous body are transformed to CaxMg2Al4+2xSi5−xO18 fibers when a ratio of 76.8% mullite fibers:6.2% Isofrax fibers: 17% bentonite clay is mixed together; whereas about 10% of the fibers within a fibrous body are transformed to CaxMg2Al4+2xSi5−xO18 fibers when a ratio of 91% mullite fibers:3.8% Isofrax fibers:5.1% bentonite clay is used.

With the ability to control fiber chemistry and crystal structure, the fibrous material can be tailored to provide a low CTE value. For example, cordierite, Mg2Al4Si5O18, is known to have a relatively low average CTE value (1×10−6/° C.). However, by modifying cordierite's chemistry (RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18) and crystal structure, lower CTE values, especially in a particular lattice direction can be achieved. Moreover, by providing fiber alignment within the fibrous material, further tailoring of the material's CTE value can be achieved.

The fibrous materials resulting from methods 100 and 200 can be shaped into porous honeycomb substrates or bodies, which can be utilized as filters and in particular, filters for automotive applications.

Referring to FIG. 5, a porous honeycomb body 510 is shown. The honeycomb body 510 has an array of walls 515 that define channels 520 between adjacent walls 515. The walls 515 comprise the fibrous material described above. That is, the walls 515 include a plurality of either RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers bonded to form a porous structure. The porous structure has at least 20% porosity and typically has an open-network of pores so that fluids can flow through the structure. At least 20% of the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 fibers within the walls 515 are aligned. As a result, material properties, such as the coefficient of thermal expansion, which have directional values, can be manipulated to provide a lower value in a particular direction. That is, the fibers can be aligned along a particular lattice direction, such as the lattice parameter (a, b, or c) which has the lowest CTE value. For example, if a particular material has the lowest CTE along the c direction, then the fibers can be extruded or otherwise shaped such that at least 20% (e.g., 25%, 30%, 40%, 50%, 60%, 70%, 80%, 90%) of the fibers are substantially aligned along the c direction. The walls of the honeycomb body 510 can then be formed such that the c direction of the aligned fibers falls within the plane of the walls 515. As a result, the walls will experience the least amount of expansion when exposed to heat. Similarly, the fibers in the material can be aligned such that 20% or more (e.g., 25%, 30%, 40%, 50%, 60%, 70%, 80%) of the fibers are aligned along a direction that has the highest CTE value. In this embodiment, the walls 515 of the honeycomb body 510 are formed such that the aligned fibers form the smallest dimension (i.e., depth) of the walls 515 so that the area greatest affected by heat is positioned to have the least structural effect.

The honeycomb body 510 can be fabricated in any number of shapes such as, for example, a cylinder (shown in FIG. 5), a pie-shaped wedge or subcylindrical section, a rectangle (as shown in FIG. 6), or a diamond. These honeycomb bodies 510 can be glued together to form a segmented body as shown in FIG. 6. As a result of gluing the bodies together, any size, shape, or dimension honeycomb form can be generated. With a low coefficient of thermal expansion porous fibrous material, it is possible to extrude or otherwise form shapes (e.g., cylinders) with large widths (e.g., diameters between 5.66 inches and 14 inches) without utilizing a low Young's modulus glue/adhesive to adjoin smaller segments to form a larger form. The ability to extrude or form larger widths provides flexibility in production techniques and potential cost reduction in volume production.

FIG. 7 depicts a cross-sectional representation of a filter 700 utilizing the porous honeycomb body 510 of FIG. 5. The filter 700 includes a housing 720, which surrounds the porous honeycomb body 510. The housing includes an inlet 705 and an outlet 707 through which gasses, such as exhaust gasses, travel through. Between the housing 720 and the honeycomb body 510 is a mat 730 that supports and forms an air-tight seal between the housing 720 and the honeycomb body 510. The honeycomb body 510 is configured in a wall-flow configuration by selectively plugging alternate channels, with outlet blocks 760 and inlet blocks 770 to form a plurality of respective inlet channels 740 and outlet channels 750. In this embodiment, the open network of pores within the walls 515 provides sufficient porosity and permeability to permit flow through the walls 515 between the inlet and outlet channels 740, 750. As a result, particulate matter can be accumulated on the surface of the inlet channel walls 740, and be removed from the gas stream by means of the filter 700. Coatings, such as, catalytic coatings or other reactive coatings, can be deposited along the walls 515 to increase the concentration of particles captured by the walls 515. For example, for a filter used in a diesel automotive environment, the walls 515 can be coated with a catalytic coating that facilitates oxidation of accumulated soot and accelerates the conversion of exhaust gas into less-harmful constituents. Techniques for applying catalytic and other types of coatings to substrates and porous bodies are well known in the field of art.

FIG. 8 illustrates a method of forming a honeycomb body, such as honeycomb body 510 of FIG. 5. First, as shown in step 810, at least two RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors wherein one or more of the precursors is in fiber form are mixed together to form a mixture. Fluid, pore formers, and/or rheology agents such as binders can also be added to the mixture to enable efficient extrusion or shaping of the mixture. After obtaining a desired consistency, the mixture is extruded into a honeycomb body having at least 20% porosity (step 820) and then heated to react the at least two RxMg2Al4+2xSi5−xO18 RxMg2−xAl4Si5O18 precursors and to substantially eliminate or remove the optional additives (i.e., fluids, pore formers, and binders (step 830)). At least 5% of all of the fibers within the honeycomb body are transformed to have either the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure. Bonds between fibers (i.e., between the fibers formed from the precursors in step 830 and any unreacted fibers) are formed via sintering 840 the honeycomb body. In some embodiments, steps 830 and 840 occur during one heat treatment process. In other embodiments, multiple heat treating processes are utilized to react the RxMg2Al4+2xSi5−xO18 or RxMg2−xAl4Si5O18 precursors, to substantially eliminate optional additives, and to sinter fibers. In embodiments where the honeycomb body is a filter, inlet and outlet blocks (e.g., 740, 750 in FIG. 7) are inserted to create a flow path through the filter (optional step 850). In addition, a catalytic coating can be applied to the filter to provide the filter with reactive functionality in its intended application, such as, for example, to promote oxidation of captured soot in a diesel particulate filter (optional step 860).

Variations, modifications, and other implementations of what is described herein will occur to those of ordinary skill in the art without departing from the spirit and scope of the invention. For example, while an number of embodiments have been described in which the fibrous material has been utilized as a filter, especially a filter for diesel applications, the fibrous material can be used in any application where a low coefficient of thermal expansion ceramic material would be desired, such as for example, in the aerospace industry, liquid filtration, cross flow filtration, molten metal filtration, fixed bed chemical reactors, honeycomb high surface area adsorbents, and high temperature reactors.

EXAMPLES

The following examples are provided to further illustrate and to facilitate the understanding of the disclosure. These specific examples are intended to be illustrative of the disclosure and are not intended to be limiting.

In a first illustrative example in which the target fiber chemistry is CaxMg2Al4+xSi5−xO18 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 71.2 grams of mullite fibers, 21.9 grams of Isofrax fibers, 5.3 grams of MgCO3 particles, and 1.5 grams of CaCO3. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose (an organic binder and rheology modifier), 65 grams of carbon particles (−45 micron mesh grade and utilized as a pore former), and 130 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 88% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca0.1Mg2Al4.1Si4.9O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.8×10−6/° C. and the fibers are observed to be approximately 70-80% aligned in the extrusion direction.

In a second illustrative in which the target fiber chemistry is CaxMg2Al4+xSi5−xO18 (where x=1.0) with a triclinic crystal structure, the following precursors are mixed together: 62 grams of mullite fibers, 18.6 grams of Isofrax fibers, 6.9 grams of MgCO3 particles, and 12.5 grams of CaCO3. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (−45 micron mesh grade), and 130 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 89% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca1Mg2Al3Si4O18 fibers having a triclinic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7×10−6/° C. and the fibers are observed to be approximately 70-80% aligned in the extrusion direction.

In a third illustrative example in which the target fiber chemistry is CaxMg2Al4+xSi5−xO18 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 96 grams of mullite fibers, 2.0 grams of Isofrax fibers, 2.0 grams of MgCO3 particles, and 0.6 grams of CaCO3. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), and 70 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 77% porosity. Approximately 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca0.1Mg2Al4.1Si4.9O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 3.2×10−6/° C.

In a third illustrative example in which the target fiber chemistry is CaxMg2Al4+xxSi5−xO18 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 161.8 grams of mullite fibers, 13 grams of Isofrax fibers, and 35.9 grams of bentonite clay. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (−45 micron mesh grade), and 130 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 75% porosity. Approximately, 45% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca0.1Mg2Al4.1Si4.9O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7×10−6/° C.

In a fourth illustrative example in which the target fiber chemistry is CaxMg2Al4+xxSi5−xO18 (where x=0.1) with an orthorhombic crystal structure, the following precursors are mixed together: 53.2 grams of mullite fibers, 2.2 grams of Isofrax fibers, and 3 grams of bentonite clay. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 65 grams of carbon particles (−45 micron mesh grade), and 60 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 86% porosity. Approximately, 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ca0.1Mg2Al4.1Si4.9O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 3.1×10−6/° C.

In a fifth illustrative example in which the target fiber chemistry is Ge0.8Mg2Al4.8Si4.2O18 with an orthorhombic crystal structure, the following precursors are mixed together: 59.8 grams of alumina silicate fibers, 6 grams of Isofrax fibers, and 11.1 grams of GeO2 particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), 23.2 grams of MgCO3 as binder, and 130 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 85% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Ge0.8Mg2Al4.8Si4.2O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7×10−6/° C.

In a sixth illustrative example in which the target fiber chemistry is Mn1Mg1Al4Si5O18 with an orthorhombic crystal structure, the following precursors are mixed together: 63.8 grams of alumina silicate fibers, 19.8 grams of Isofrax fibers, and 11.9 grams of MnO particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), 4.6 grams of MgCO3 as binder, and 70 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 82% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Mn1Mg1Al4Si5O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.6×10−6/° C.

In a seventh illustrative example in which the target fiber chemistry is K0.5Mg2Al4.5Si4.5O18 with an orthorhombic crystal structure, the following precursors are mixed together: 71.2 grams of alumina silicate fibers, 2.3 grams of Isofrax fibers, and 1.2 grams of K2O particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), 25 grams of MgCO3 as binder, and 70 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio- frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 86% porosity. More than 80% of all of the alumina silicate fibers and Isofrax fibers utilized in the extrudable mixture reacted to form K0.5Mg2Al4.5Si4.5O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.8×10−6/° C.

In an eight illustrative example in which the target fiber chemistry is K0.5Mg2Al4.5Si4.5O18 with an orthorhombic crystal structure, the following precursors are mixed together: 49.4 grams of mullite fibers, 39.6 grams of Isofrax fibers, and 1.2 grams of K2O particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), 9.7 grams of MgCO3 as binder, and 70 grams of deionized water as a mixing fluid. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 89% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form K0.5Mg2Al4.5Si4.5O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7×10−6/° C.

In a ninth illustrative example in which the target fiber chemistry is Fe0.45Mg1.55Al4Si5O18 with an orthorhombic crystal structure, the following precursors are mixed together: 42 grams of mullite fibers, 46.9 grams of Isofrax fibers, and 11.1 grams of Fe2O3 particles. The following additives are also added to form an extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), and 70 grams of deionized water. The materials are mixed into the extrudable mixture and formed into 1″ diameter honeycomb substrates by extrusion. The substrates are dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 87% porosity. More than 80% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Fe0.45Mg1.55Al4Si5O18 fibers having an orthorhombic crystal structure. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 0.7×10−6/° C.

In a tenth illustrative example, the targeted fiber chemistry is a modified cordierite structure which includes 10% cordierite fibers with 90% alumina silicate fibers. Thus, in this example there is no R to modify the cordierite structure, however modification from the cordierite structure is achieve by having less than 95% conversion of the precursor materials so that the ultimate fiber chemistry is a blend of cordierite and alumina silicate. The 90% alumina silicate with 10% cordierite fibrous material is prepared by mixing the following precursor materials to form an extrudable mixture: 96 grams of mullite fibers, 2.0 grams of Isofrax fibers, and 2.0 grams of MgCO3 particles. The following additives are also added to the extrudable mixture: 16 grams of hydroxypropyl methylcellulose, 20 grams of carbon particles (−45 micron mesh grade), and 70 grams of deionized water. The materials are mixed and extruded to form 1″ diameter honeycomb substrate. The substrate is dried using a radio-frequency (RF) drying facility, followed by a sintering operation at 1,300° C. for two hours to form a porous honeycomb structure having about 77% porosity. Only 10% of all of the mullite fibers and Isofrax fibers utilized in the extrudable mixture reacted to form Mg2Al4Si5O18 fibers. In this embodiment, the coefficient of thermal expansion of the porous ceramic body is 2.8×10−6/° C.

Claims (22)

1. A method of manufacturing a fibrous material wherein at least about 5% of all fibers within the fibrous material have a RxMg2Al4+xSi5−xO18 compositional structure or a RxMg2−xAl4+xSi5O18 compositional structure, the method comprising:

mixing at least two RxMg2Al4+xSi5−xO18 precursor materials or RxMg2−xAl4Si5O18 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is in a form of a fiber;

extruding the mixture to create a fibrous body; and

heat treating the fibrous body to form the fibrous material wherein x is greater than zero and R is an element other than Mg, Al, Si, or O.

2. The method of claim 1 wherein after heat treating at least about 25% of all fibers within the fibrous body have either the RxMg2Al4+xSi5−xO18 compositional structure or the RxMg2−xAl4Si5O18 compositional structure.

3. The method of claim 1 wherein one or more of the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is selected from the group consisting of: magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.

4. The method of claim 1 wherein the mixture further comprises one or more additives selected from the group consisting of a fluid, a binder, and a pore former.

5. The method of claim 4 wherein the one or more additives are substantially removed by heating the fibrous body.

6. A method of manufacturing a fibrous body including RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibers, the method comprising:

mixing at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is in a form of a fiber;

reacting the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a plurality of fibers within the mixture that have RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure; and

shaping the mixture into the fibrous body, wherein at least about 5% of all fibers within the fibrous body have either the RxMg2Al4+xSi5−xO18 compositional structure or the RxMg2−xAl4Si5O18 compositional structure wherein x is greater than zero and R is an element other than Mg, Al, Si, or O.

7. The method of claim 6 wherein at least about 25% of all fibers within the fibrous body after reacting the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials have the RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure, respectively.

8. The method of claim 6 wherein at least about 20% of all fibers within the fibrous body are aligned in a common direction.

9. The method of claim 6 wherein one or more of the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is selected from the group consisting of: magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.

10. The method of claim 6 wherein the mixture further comprises one or more additives selected from the group consisting of a fluid, a binder, and a pore former.

11. The method of claim 10 wherein the one or more additives are substantially removed by heating the fibrous body.

12. A method of forming a porous honeycomb substrate, the method comprising:

mixing at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a mixture, wherein one or more of the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is in a form of a fiber;

extruding the mixture to form a honeycomb substrate having a porosity of at least about 20%; and

heat treating the honeycomb substrate to react the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials to form a plurality of fibers having RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure so that at least about 5% of all fibers within the honeycomb substrate have the RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure wherein x is greater than zero and R is an element other than Mg, Al, Si, or O.

13. The method of claim 12 wherein after heat treating the honeycomb substrate at least about 25% of all fibers have the RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 compositional structure.

14. The method of claim 12 wherein one or more of the at least two RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 precursor materials is selected from the group consisting of: magnesia silica fibers, magnesium aluminate fibers, and alumina silicate fibers.

15. The method of claim 12 wherein the mixture further comprises one or more additives selected from the group consisting of a fluid, a binder, and a pore former.

16. The method of claim 15 wherein the one or more additives are substantially removed by heating the honeycomb substrate.

the walls comprising a plurality of RxMg2Al4−xSi5−xO18 or RxMg2−xAl4Si5O18 fibers bonded to form a porous structure having an open network of pores, wherein at least about 20% of the plurality of RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibers within the walls being aligned in a common direction wherein x is greater than zero and R is an element other than Mg, Al, Si, or O.

18. The RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibrous honeycomb body of claim 17, wherein the walls have a porosity of at least about 20%.

19. The RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibrous honeycomb body of claim 17 wherein the plurality of RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibers have an aspect ratio greater than 1 and less than or equal to 2,000.

20. The RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibrous honeycomb body of claim 17 further comprising a catalytic coating on the plurality of RxMg2Al4+xSi5O18 or RxMg2−xAl4Si5O18 fibers.

21. A filter comprising:

a housing including an inlet and an outlet; and

the RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibrous honeycomb body of claim 17 disposed between the inlet and the outlet.

22. The filter of claim 21 further comprising at least one catalyst deposited on the plurality of RxMg2Al4+xSi5−xO18 or RxMg2−xAl4Si5O18 fibers of the walls.